2020
DOI: 10.1016/j.actaastro.2020.06.016
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Short-term space safety analysis of LEO constellations and clusters

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Cited by 22 publications
(6 citation statements)
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“…The short-term collision probability orbit prediction model uses the SGP4 model to simulate the first phase of the Starlink constellation and to facilitate the prediction of the orbit of the space cataloging target [30]. The constellation parameters of the first phase of Starlink are 1584/72/33, the orbit inclination is 53°, and the orbit height is 550 km.…”
Section: Numerical Experimental Setupmentioning
confidence: 99%
“…The short-term collision probability orbit prediction model uses the SGP4 model to simulate the first phase of the Starlink constellation and to facilitate the prediction of the orbit of the space cataloging target [30]. The constellation parameters of the first phase of Starlink are 1584/72/33, the orbit inclination is 53°, and the orbit height is 550 km.…”
Section: Numerical Experimental Setupmentioning
confidence: 99%
“…Large clusters of derelict LEO rocket bodies have been identified as high priority candidates for future ADR missions (Liou 2011;Rossi et al 2020;McKnight et al 2021;Maclay & Mcknight 2021). Another key target is ESA's defunct eight-tonne satellite, Envisat, which resides in a densely populated region and is known to be tumbling (Kucharski et al 2014;Pittet et al 2018).…”
Section: Fixes For the Futurementioning
confidence: 99%
“…Simulations of the long-term evolution of debris suggest that LEO is already in the protracted initial stages of the Kessler Syndrome but that this could be managed through active debris removal [ 25 ]. The addition of satellite mega-constellations and the general proliferation of low-cost satellites in LEO stresses the environment further [ 26 , 27 , 28 ]. Hence, decades of the world’s space activities have left LEO cluttered with active satellites and littered with orbital debris.…”
Section: Introductionmentioning
confidence: 99%